A Problem in Matching an Inlet and Engine Having Steady-State Circumferential Inlet Pressure Distortion,
Abstract
An analysis was made of the flow redistribution which occurs at the exit of an inlet due to the presence of a compressor. The flow redistribution includes a change in the axial velocity distortion, which is a function of the slope of the curve of compressor pressure coefficient versus flow coefficient at a particular corrected speed. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1970
- Accession Number
- AD0875187
Entities
People
- Donald F. Brunda